| 000 | 00657pam a2200205a 44500 | ||
|---|---|---|---|
| 005 | 20200227151620.0 | ||
| 008 | 200227b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 100 | _aMercer, J. E. | ||
| 245 | 1 |
_aAerodynamics influence coefficient method using singularity splines [NASA CR-2423] _cJ. E. Mercer, J. A. Weber and E. P. Lesferd |
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| 260 |
_bNASA _cMay 1974 _aWashington, D. C. |
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| 300 | _a100p | ||
| 440 | _aNational Aeronautics and Space Administration (NASA) | ||
| 505 | _aNASA contractor report | ||
| 650 | _aAerodynamic influence | ||
| 700 | _aWeber, J. A.. | ||
| 700 | _aLesferd, E. P. | ||
| 942 | _cBK | ||
| 999 |
_c394237 _d394237 |
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